Aircraft Engineering and Aerospace Technology: Volume 15 Issue 12
Strapline:
An International JournalTable of contents
THE SHEET METAL PROCESS
JUST over a year ago (in the October and November 1942 issues of AIRCRAFT ENGINEERING) we published an Institute of the Aeronautical Sciences paper by Mr. F. R. SHANLEY of the…
Airscrew Blade Twist Effects
J. Lockwood TaylorORDINARILY, for the purpose of strength calculations, as well as in estimating bending and torsional rigidity with a view to deriving blade deflections and investigating flutter…
Rectangular Tubes under Torque
J. RatzersdorferLET us consider a tube of length L of doubly symmetrical rectangular cross section, built‐in or simply supported at one end and free at the other. The tube is affected by…
The Lateral Stability of Aeroplanes: Derivative Calculation by the Lotz System
H.L. PriceSYMMETRIC AND ANTI‐SYMMETRIC WING LOADING DISTRIBUTIONS IT is proposed to work out the span loading distribution and lift and drag coefficients of an unstalled wing in symmetric…
Foreign Research Progress: Translations Issued by the N.A.C.A.
The present report deals with a number of problems, particularly with the interaction of the fuse‐lage with the wing and tail, on the basis of simple calculating methods derived…
Sheet‐Metal Forming and Assembling
William Schroeder, Thomas H. HazlettTHE modern aeroplane is constructed largely from sheet metal. As such, the most important production problems are those of sheet metal forming, and assembling. Production is here…
U.S. Patent Specifications
In a vehicle power plant comprising a pair of coaxial controllable‐pitch propellers and means for rotating said propellers independently in opposite directions, means for holding…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb